English
Volume II contains the tabulated data obtained during Test Number 1 and 2 at AEDC and Tests Number 3, 4, and 5 at NASA Langley Research Center.
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ई-पुस्तक · DTIC ADB010054: A Compilation of Static Stability and Fin Loads Data for Slender Body Missile Models with and without Tail Fins and Wings. Volume 2. Appendixes A through E. Tests Number 1 through 5 · Defense Technical Information Center · Internet Archive
DTIC Archive · Gomillion, G R · ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AFB TN · *GUIDED MISSILE MODELS · AERODYNAMIC CHARACTERISTICS · AERODYNAMIC CONTROL SURFACES · AERODYNAMIC FORCES · AERODYNAMIC LOADING · ANGLE OF ATTACK · DEFLECTION